34th Congress of the International Council of the Aeronautical Sciences

05 - Propulsion

MULTI-DIMENTIONAL DESIGN AND THERMAL PROTECTION CAPABILITY OF A REGENERATIVE COOLED RBCC VARIABLE-GEOMETRY COMBUSTOR

L. Zhang, China; T.-T. Jing, China; X. Sun, China; T. Gao, China; Z. Xu, China; F. Qin, China

The study conducted a multidimensional approach to design the regenerative cooling structure of the RBCC variable-geometry combustor. The investigation aimed to determine the effect of different cooling equivalent ratios on the cooling effect.


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